8,
Approach Speed
-
8%.
MPH
(7%.
Kts)
%AS.
9.
Master Switch
-
OFF,
Prior to Landing.
Up
to
2000
feet
of
altitude may be lost in
a
one turn spin and
recovery; therefore, stalls at low altitude are extremely
criticaA
The best spin recovery technique
is
to avoid flight conditions
conducive to
spin
entry.
Low speed flight near stall should
be approached with caution and excessive flight control
move--
ments
in
this RligM regime should be avoided,
Shuuld
an
amintentional stall occur the aircraft should not be all.owed
to progress into
a
deep stall. Fast, brat smooth stall recovery
will
mininiize the risk of progressing into
a
spin, If an
unusual post
shall attitude develops and results in
a
spin,
quick
application of anti
-
spin procedures should shorten the
PeCOTJ6?Prys
IN'TENTIQNAE
SPINS
ARE
PROHIBITED.
In
the event of
an
inadvertent spin, the following recovery procedure sfaorald
be used:
1,
Rudder
-
Apply
FULL
RUDDER
opposite the direction
of spin,
2,
Control Wheel
-
FORWARD of neutral in
a
brisk motion.
Additional FORWARD elevator control may
be
required
if
the rotation does not stop.
3.
Ailerons
-
NE
UTRAL.
4.
Throttle
-
RETARD
TO
IDLE.
Hold anti
-
spin co&roRs until rotation stops:
5,
Fbps
-
Bf
edended, RETRACT as soon
as
possible.
6.
Rudder
-
NEmMUZE,
7.
Control Wheel
-
Smoothly move
aft
to bring the nose
up to
a
level flight attitude,
ISSUED
XI-
15
-
77
REV
@
9
-
29
-
82
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